EP3039275A4 - Thrust reverser sliding door assembly - Google Patents

Thrust reverser sliding door assembly Download PDF

Info

Publication number
EP3039275A4
EP3039275A4 EP14860314.5A EP14860314A EP3039275A4 EP 3039275 A4 EP3039275 A4 EP 3039275A4 EP 14860314 A EP14860314 A EP 14860314A EP 3039275 A4 EP3039275 A4 EP 3039275A4
Authority
EP
European Patent Office
Prior art keywords
sliding door
door assembly
thrust reverser
reverser sliding
thrust
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP14860314.5A
Other languages
German (de)
French (fr)
Other versions
EP3039275A2 (en
EP3039275B1 (en
Inventor
Mike Charron
Robert L. Gukeisen
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of EP3039275A2 publication Critical patent/EP3039275A2/en
Publication of EP3039275A4 publication Critical patent/EP3039275A4/en
Application granted granted Critical
Publication of EP3039275B1 publication Critical patent/EP3039275B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
    • F02K1/605—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers the aft end of the engine cowling being movable to uncover openings for the reversed flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/02—Power-plant nacelles, fairings, or cowlings associated with wings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/70—Disassembly methods
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/72—Maintenance
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/80—Repairing, retrofitting or upgrading methods
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/50—Kinematic linkage, i.e. transmission of position
EP14860314.5A 2013-08-28 2014-08-14 Thrust reverser sliding door assembly Active EP3039275B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201361870829P 2013-08-28 2013-08-28
PCT/US2014/051003 WO2015069350A2 (en) 2013-08-28 2014-08-14 Thrust reverser sliding door assembly

Publications (3)

Publication Number Publication Date
EP3039275A2 EP3039275A2 (en) 2016-07-06
EP3039275A4 true EP3039275A4 (en) 2017-05-17
EP3039275B1 EP3039275B1 (en) 2020-03-04

Family

ID=53042291

Family Applications (1)

Application Number Title Priority Date Filing Date
EP14860314.5A Active EP3039275B1 (en) 2013-08-28 2014-08-14 Thrust reverser sliding door assembly

Country Status (3)

Country Link
US (1) US10221809B2 (en)
EP (1) EP3039275B1 (en)
WO (1) WO2015069350A2 (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160305370A1 (en) * 2015-04-16 2016-10-20 Honeywell International Inc. Translating cowl thrust reverser with door pivots aft of reverse flow path
FR3047973B1 (en) * 2016-02-23 2018-03-09 Airbus Operations AIRCRAFT ENGINE ASSEMBLY, COMPRISING A MOTOR ATTACHING DEVICE EQUIPPED WITH STRUCTURAL MOBILE HOOKS CONNECTED TO THE CENTRAL CABIN
US10267262B2 (en) 2016-05-06 2019-04-23 Mra Systems, Llc Thrust reverser assembly
US10563614B2 (en) 2016-08-17 2020-02-18 Honeywell International Inc. Composite translating cowl assembly for a thrust reverser system
US10118650B1 (en) 2017-07-27 2018-11-06 Cnh Industrial America Llc Engine access door slide track system
EP3668791B1 (en) 2017-11-10 2022-06-15 Donaldson Company, Inc. Airflow control system and methods thereof
FR3076323B1 (en) * 2017-12-28 2020-01-10 Safran Nacelles GRID DRIVER INVERTER FOR TURBOJET
FR3089207A1 (en) 2018-11-30 2020-06-05 Airbus Operations propulsion system of an aircraft comprising a movable and articulated hood
US20200172255A1 (en) * 2018-12-04 2020-06-04 Goodrich Corporation Guided fan cowl hinge
US11204037B2 (en) 2018-12-21 2021-12-21 Rolls-Royce Plc Turbine engine
US10995701B2 (en) 2019-09-05 2021-05-04 Rohr, Inc. Translating sleeve thrust reverser assembly
US11754019B2 (en) 2021-12-17 2023-09-12 Rohr, Inc. Articulating slider for nacelle

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008045062A1 (en) * 2006-10-12 2008-04-17 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle with sliding actuation system
US20130075492A1 (en) * 2011-03-02 2013-03-28 Spirit Aerosystems, Inc. Thrust reverser translating sleeve assembly

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4183478A (en) * 1977-11-25 1980-01-15 The Boeing Company Jet thrust reverser
FR2638783B1 (en) 1988-11-10 1991-04-05 Astech PUSH INVERTER, ESPECIALLY FOR AN AIRCRAFT REACTION ENGINE
US5083426A (en) 1989-10-02 1992-01-28 Rohr Industries, Inc. Integrated engine shroud for gas turbine engines
US5915765A (en) * 1998-03-17 1999-06-29 The Boeing Company Opposing hook latch
US6340135B1 (en) 2000-05-30 2002-01-22 Rohr, Inc. Translating independently mounted air inlet system for aircraft turbofan jet engine
US6845945B1 (en) 2001-07-20 2005-01-25 Aircraft Integration Resources, Inc. Thrust reverser with sliding pivot joints
US6584763B2 (en) 2001-08-01 2003-07-01 Rohr, Inc. Lock for the translating sleeve of a turbofan engine thrust reverser
US6568172B2 (en) 2001-09-27 2003-05-27 The Nordam Group, Inc. Converging nozzle thrust reverser
US6684623B2 (en) * 2002-02-27 2004-02-03 Honeywell International, Inc. Gearless electric thrust reverser actuators and actuation system incorporating same
FR2897339B1 (en) * 2006-02-16 2008-04-11 Aircelle Sa NACELLE DE TURBOREACTEUR WITH LATERAL OPENING OF HOODS
AT503290B1 (en) 2006-06-23 2007-09-15 Fischer Adv Components Gmbh Guide rail for cowling of turbo jet engine of aircraft, has base body formed by hollow profiled unit, where hollow profiled unit is produced from carbon-fibre reinforced plastic material according to resin infusion method
FR2914700B1 (en) * 2007-04-04 2009-05-22 Aircelle Sa THRUST INVERTER FOR REACTION ENGINE
US8959889B2 (en) * 2008-11-26 2015-02-24 The Boeing Company Method of varying a fan duct nozzle throat area of a gas turbine engine
US8109467B2 (en) * 2009-04-24 2012-02-07 United Technologies Corporation Thrust reverser assembly with shaped drag links
US8869507B2 (en) 2010-01-13 2014-10-28 United Technologies Corporation Translatable cascade thrust reverser
FR2959488B1 (en) 2010-04-28 2012-05-18 Aircelle Sa NACELLE FOR AN AIRCRAFT ENGINE WITH THRUST INVERTER WITH GRIDS AND ADAPTIVE TUBE
FR2974150B1 (en) * 2011-04-14 2013-04-12 Aircelle Sa THRUST INVERTER FOR AIRCRAFT TURBOREACTOR

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008045062A1 (en) * 2006-10-12 2008-04-17 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle with sliding actuation system
US20130075492A1 (en) * 2011-03-02 2013-03-28 Spirit Aerosystems, Inc. Thrust reverser translating sleeve assembly

Also Published As

Publication number Publication date
WO2015069350A2 (en) 2015-05-14
US20160201600A1 (en) 2016-07-14
WO2015069350A3 (en) 2015-07-16
US10221809B2 (en) 2019-03-05
EP3039275A2 (en) 2016-07-06
EP3039275B1 (en) 2020-03-04

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